Precipitative static drain strip system

A device for dissipating static charge collected in the surface of an aircraft window having a plurality of electroconductive film (32, 34, 38) elements on the outboard surface (28) of the aircraft window. The elements (32, 34, 38) are electrically interconnected and grounded such that charges accum...

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Bibliographic Details
Main Authors HORNSEY, WILLIAM WALTER, MUELLER, JOSEPH TIMOTHY
Format Patent
LanguageEnglish
French
German
Published 03.05.1989
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
ELECTRICITY
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
NATURALLY-OCCURRING ELECTRICITY
PARACHUTES
PERFORMING OPERATIONS
STATIC ELECTRICITY
TRANSPORTING
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Summary:A device for dissipating static charge collected in the surface of an aircraft window having a plurality of electroconductive film (32, 34, 38) elements on the outboard surface (28) of the aircraft window. The elements (32, 34, 38) are electrically interconnected and grounded such that charges accumulated by the film elements (32, 34, 38) passed there along to the ground. An electrical window heating system may be incorporated into the plies of the window.
Bibliography:Application Number: EP19880117957